View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59374U 26145.57785668 +.00000000 +00000-0 +37857-4 0 00005
2 59374 53.1599 260.6426 0000938 94.7418 265.3692 15.34385238 06
| Epoch (UTC): | 25 May 2026 13:52:06 |
| Eccentricity: | 0.0000938 |
| inclination: | 53.1599° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 260.6426° |
| argument of perigee: | 94.7418° |
| revolutions per day: | 15.34385238 |
| mean anomaly at epoch: | 265.3692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|